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Effects of wing leading-edge deflection on the low-speed aerodynamic characteristics of a low-aspect-ratio highly swept arrow-wing configuration
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Weston, R. P. Coe Jr., P. L. |
| Copyright Year | 1978 |
| Description | Wing leading-edge deflection effects on the low-speed aerodynamic characteristics of a low-aspect-ratio highly swept arrow-wing configuration were determined. Static force tests were conducted in a V/STOL tunnel at a Reynolds number of about 2.5 x 1 million for an angle-of-attack range from -10 deg to 17 deg and an angle-of-sideslip range from -5 deg to 5 deg. Limited flow visualization studies were also conducted in order to provide a qualitative assessment of leading-edge upwash characteristics. |
| File Size | 5568134 |
| Page Count | 67 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19780025104 |
| Archival Resource Key | ark:/13960/t8nd0rq8d |
| Language | English |
| Publisher Date | 1978-09-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Arrow Wings Swept Wings Low Aspect Ratio Wings Wind Tunnel Stability Tests Aerodynamic Characteristics Leading Edges Flow Deflection Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |